I - Model CITATION (Transport Category), approved 09 October 1998.
|
|
- Anne Walters
- 6 years ago
- Views:
Transcription
1 TYPE CERTIFICATE DATA SHEET Nº EA-9810 Type Certificate Holder: CESSNA AIRCRAFT CO. P. O. Box 7704 Wichita, Kansas, USA EA Sheet 01 CESSNA CITATION 750 X 10 October 2011 This data sheet, which is part of Type Certificate No prescribes conditions and limitations under which the product, for which the Type Certificate was issued, meets the airworthiness requirements of the Brazilian Aeronautical Regulations. I - Model CITATION (Transport Category), approved 09 October ENGINE For airplane serial numbers through not incorporating Cessna Service Bulletin SB : - Two Rolls-Royce Model AE 3007C, P/N Engines controlled by (2 each engine) Full Authority Digital Electronic Control (FADEC). Approved FADEC P/N are the following: FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C9 For airplanes serial numbers and on and aircraft incorporating Cessna Service Bulletin SB : - Two Rolls-Royce Model AE 3007C1, P/N Engines controlled by (2 each engine) Full Authority Digital Electronic Control (FADEC). Approved FADEC P/N are the following: FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C FADEC Version C9
2 CESSNA 10 October 2011 EA Sheet 2/9 FUEL Jet A, Jet A-1 and Jet B per ASTM D 1655, Jet Fuel No. 3 (GB ), JP-4 and JP-5 per MIL-T5624, JP-8 per MIL-T-83133, NATO F34, F35,F40,F43 and F44. EGME (ASTM D 4171, Class 1, or MIL- I-27686) or DIEGME (ASTM D 4171, class 3, or MIL-I-85470) antiicing additive may be blended into the aircraft fuel in concentrations of not more than 0.15 percent by volume. Mixtures of EGME and DIEGME are permissible if combined concentrations are within limits. JP-5, JP-8, F34 and F44 fuels may have anti-icing additive preblended. Hammonds Biobor JF additive is permitted up to a maximum concentration of 270 parts per million. See Airplane Flight Manual for fueling procedures. ENGINE LIMITS AE 3007C** AE 3007C1*** Static thrust, standard day, sea level: Takeoff lb lb Max. Continuous lb lb Max. permissible engine rotor operating speeds: N1 (Fan) Steady state 100% rpm 100% rpm N2 (Gas Gen.) Steady state 101.6% rpm 101.6% rpm Max. permissible interturbine gas temperatures: Takeoff (5 min. limit) 888 C / 850 o C * 907 o C Max. continuous 850 o C 857 o C Starting Started assisted 800 C 800 C Windmill 888 C / 850 o C* 888 C * For airplane serial number through no incorporating Cessna Service Bulletin SB ** For airplane serial numbers through not incorporating Cessna Service Bulletin SB *** For airplane serial numbers and on and aircraft incorporating Cessna Service Bulletin SB OIL Synthetic oil conforming to MIL-L-23699D or MIL-L-7808K (below - 40 F (- 40 C)) AIRSPEED LIMITS Maximum operating (V MO ): (CAS) (Calibrated altitudes) Sea level to m (8 000 ft) 270 kcas 2 438m (8 000 ft) to 9 342m ( ft) 350 kcas Maximum operating (M MO ): (Calibrated Altitudes) Above 9 342m ( ft) 0.92 Mach Maneuvering (V A ) - sea level: For airplane serial numbers and on and aircraft incorporating Cessna Service Bulletin SB ): kg ( lb) 233 kias All serial number kg ( lb) 221 kias kg ( lb) 217 kias kg ( lb) 202 kias kg ( lb) 193 kias
3 CESSNA 10 October 2011 EA Sheet 3/9 AIRSPEED LIMITS kg ( lb) 177 kias (CAS) (Cont.) kg ( lb) 163 kias See AFM for variations with weight and altitude and optional configurations. Maximum Gust Intensity (V A ) 300 kias (0.92 M) Flaps extended (V FE ) Stats and/or Flaps kias Flap kias Landing position - Full Flaps 180 kias (For airplane serial numbers through not incorporating Cessna Service Bulletin SB ) Minimum control speed - Air (V MCA ): 110 kias 15 flap) Minimum control speed - Ground (V MCG ): 109 kias (15 flap) (For airplane serial numbers and on and aircraft incorporating Cessna Service Bulletin SB ) Minimum control speed - Air (V MCA ): 112 kias (15 flap) Minimum control speed - Ground (V MCG ): 111 kias (15 flap) Landing Gear operating - (V LO ): 210 kias Landing Gear extended (V LE ): 210 kias Maximum tire ground speeds: Nose Gear tire 182 knots Main Gear tire 195 knots Speed Brakes Extension Speed No limit There is no restriction on roll control spoilers (panel # 1, # 2, #9 and # 10) C. G. RANGE Maximum Design C. G. limits (Landing Gear Extended) (1) Aft limits: - For airplane serial numbers through not incorporating Cessna Service Bulletin SB : 20.50% MAC from kg ( lb) to kg ( lb); linear variation from 20.50% MAC at kg ( lb) to 33.00% MAC at kg ( lb); 33% MAC at kg ( lb) to kg ( lb); linear variation from 33.0% MAC at kg ( lb) to 34.42% MAC at kg ( lb); linear variation from 34.42% MAC at kg ( lb) to 35.00% MAC at kg ( lb); 35.00% MAC at kg ( lb) to kg ( lb). - For airplane serial numbers and on and aircraft incorporating Cessna Service Bulletin SB : 20.50% MAC from kg ( lb) to kg ( lb); linear variation from 20.50% MAC at kg ( lb) to 33.00% MAC at kg ( lb); 33.0% MAC at kg ( lb) to kg ( lb); linear variation from 33.0% MAC at kg ( lb) to 34.42% MAC at kg ( lb); linear variation from 34.42% MAC at kg ( lb) to 35.00% MAC at kg ( lb); 35.00% MAC at kg ( lb) to kg ( lb).
4 CESSNA 10 October 2011 EA Sheet 4/9 C. G. RANGE (Cont.) EMPTY WEIGHT C. G. RANGE DATUM (2) Forward Limits - For airplane serial numbers through not incorporating Cessna Service Bulletin SB : linear variation from 15.84% MAC at kg ( lb) to 15.00% MAC from kg ( lb); 15.00% MAC from kg ( lb) to kg ( lb); linear variation from 15.00% MAC at kg ( lb) to 21.00% MAC kg ( lb); 21.00% MAC at kg ( lb) to kg ( lb); linear variation from 21.00% MAC at kg ( lb) to 26.16% MAC at kg ( lb); linear variation from 26.16% MAC at kg ( lb) to 35.00% MAC at kg ( lb). - For airplane serial numbers and on and aircraft incorporating Cessna Service Bulletin SB : linear variation from 16.40% MAC at kg ( lb) to 15.00% MAC at kg ( lb) to kg ( lb); linear variation from 15.00% MAC at kg ( lb) to 21.00% MAC at kg ( lb); to kg ( lb); linear variation from 21.00% MAC at kg ( lb) to 26.16% MAC at kg ( lb); linear variation from 26.16% MAC at kg ( lb) to 35.00% MAC at kg ( lb). None Zero reference datum is cm (184,5 in) forward of the leveling screw located 6.35 cm (2.50 in) forward of the cabin door frame on Water Line LEVELING MEANS Outboard floor panel inside of door parallel to B. L MEAN AERODYNAMIC CHORD cm (118.6 in) - L. E. of MAC at F. S MAXIMUM WEIGHT MINIMUM CREW MAXIMUM PASSENGERS For airplane serial numbers through not incorporating Cessna Service Bulletin SB , and not incorporating Cessna Service Bulletin SB : Takeoff: kg ( lb) Landing: kg ( lb) Zero Fuel: kg ( lb) Ramp: kg ( lb) For airplane serial numbers and on and aircraft incorporating Cessna Service Bulletin SB , or aircraft incorporating Cessna Service Bulletin SB : Takeoff: kg ( lb) Landing: kg ( lb) Zero Fuel: kg ( lb) Ramp: kg ( lb) For all flights: 2 persons (pilot and co-pilot). 12 passengers maximum. MAXIMUM BAGGAGE Tail compartment 318 kg (700 lb) at F.S
5 CESSNA 10 October 2011 EA Sheet 5/9 Floor loading density: kg per square meter (170 lb per square foot) FUEL CAPACITY Two wing tanks: usable liters (521 US Gal) each tank; arm cm ( in). Center tank: usable 3361 liters (888 US Gal) usable each tank; cm ( in). See Note 1: for data on unusable fuel. OIL CAPACITY MAXIMUM OPERATING ALTITUDE CONTROL SURFACE MOVEMENTS Two engine-mounted tanks: total 11.5 liters (12.1 qts) each; (usable) 11.2 liters. (11.8 qts) each; arm cm ( in). See Note 1 for data on unusable oil. 15,545 m (51,000 ft) To insure proper operation of the airplane, the movement of the various control surfaces must be carefully controlled by proper rigging of the flight control systems. The airplane must, therefore, be rigged in accordance with the appropriate FAA approved rigging specification or Cessna drawing. Specific rigging instructions may also be found in the Model 750 Maintenance Manual (Instructions for Continued Airworthiness), part number 75MM00 (or later approved revision). Stabilizer: Range of Stabilizer Setting (Leading Edge Position) Cessna Drawing nr Primary Trim Max. L.E. Up Max. L.E. Down Secondary Trim Max. L.E. Up Max. L.E. Down Elevator: Rigging Spec. Nr Up /-0 Down Rudder: Rigging Spec. Nr Lower (perpendicular to H. L.) Right Left Upper (perpendicular H. L.) Right /-1.0 Left /-1.0 Rudder trim: Right 11 1 Left 11 1 Aileron: Rigging Spec. Nr (from droop position) Up Down Droop position down from faired Aileron trim: Up 8 1 Down 8 1 Flaps: Cessna drawing Nr and Rigging Spec. No Flap position Nominal Outboard Nominal Center Nominal Inboard Up Full Allowable tolerance Speed break: Rigging Spec. Nr CONTROL SURFACE Panel 3, 4, 5, 6, 7 & 8 Up: 40-43
6 CESSNA 10 October 2011 EA Sheet 6/9 MOVEMENTS (Cont.) SERIAL NUMBERS ELIGIBLE IMPORT ELEGIBILITY CERTIFICATION BASIS Maximum 1.0 between corresponding panels Roll Spoilers Rigging Spec. Nr Panel 1, 2, 9 and 10 Up: and on. A Certificate of Airworthiness for Export endorsed as noted under "Import Requirements" must be submitted for each individual aircraft for which application for a Brazilian Certificate of Airworthiness is made. A Brazilian Certificate of Airworthiness may be issued on the basis of an FAA Export Certificate on Airworthiness (or a third country Export Certificate on Airworthiness, in case of used aircraft imported from such country), including the following statement: The aircraft covered by this certificate has been inspected, tested and found to be in conformity with the Brazilian approved type design as defined by the Brazilian Type Certificate no and in condition of safe operation. The CTA Report H , dated 29 October 1998 or further revisions, contains the Brazilian requirements for the acceptance of these airplanes. (See note 4) Brazilian Type Certificate Nr issued on 28 October 1998 based on the RBHA 25, which endorses the FAR Part 25 effective February 1965, as amended by 25-1 through 25-74; except the following paragraph which are in the specified amendments: Additions: RBHA/FAR (e) as amended by Amendment 25-75; and , as amended by Amendments RBHA 36, corresponding to FAR Part 36 effective 01 December 1969 as amended by Amendment 36-1 through plus Noise Control Act of RBHA 34, corresponding to FAR 34 effective 10 September Special Conditions as follows. No. 25-ANM-80, additional requirements for High Altitude Operation (see note 8). No. 25-ANM-99, additional requirements for protection of Electrical and Electronic Systems from High Intensity Radiated Fields (HIRF) No. 25-ANM-113, additional requirements for operation with Fly-by- Wire Rudder Equivalent levels of safety, accepted by ANAC relative to the following requirements: CERTIFICATION BASIS RBHA/FAR (d) and , Design Discrete Gust Criteria; RBHA/FAR (e) (4), Red Arrow Marking for the Main Passenger Door Handle; RBHA/FAR (e), Ditching Emergency Exits for Passenger; RBHA/FAR (b) (6), Cabin Pressurization - High Altitude Take-off and Landing Operations; RBHA/FAR (a) & (c), Digital Turbine Speed; RBHA/FAR , Digital APU Indicators (Oil Pressure, Oil Temperature, Gas Temperature, Tachometer);
7 CESSNA 10 October 2011 EA Sheet 7/9 (Cont.) RBHA/FAR , , , , , and Accelerate-Stop Distance; RBHA/FAR (d) (1) and (b) (1) (i), Emergency Exit Locator Signs; RBHA/FAR , and , Stall Warning System for flight conditions above feet; and RBHA/FAR (e). Emergency Exit Excess Exemptions, accepted by ANAC relative to the following requirements: No. 6179, exemption from bird impact requirements of RBHA/FAR (e) (1); No. 6431, exemption from Engine-out lateral trim requirements of RBHA/FAR (d): and No. 6432, exemption from the emergency landing dynamic conditions of RBHA/FAR for multiple-occupancy, sidefacing divans. Expires 30 November 1996; or No. 7922, Partial grant of exemption from the general occupant protection requirements of RBHA/FAR (b) for multipleoccupancy, side facing divans, restricted to airplanes manufactured prior to 01 January No. 7922A, exemption from the general occupant protection requirements of RBHA/FAR (b) for multiple-occupancy, side-facing divans, (no restriction). RBHA/ FAR ditching not complied with. Compliance with ice protection has been demonstrated in accordance with RBHA/FAR Application for Brazilian Type Certificate dated 10 April PRODUCTION CERTIFICATION Production Certificate No. 4 amended to add Model 750 effective 04 October See note 7 for applicable airplane serial numbers. REQUIRED EQUIPMENT The basic required equipment, as prescribed in the applicable airworthiness regulations (see Certification Basis), must be installed in the airplane. NOTES: NOTE 1 The approved Weight and Balance Manual: part number 75WB-01 (or later approved revision) is applicable to the model 750 serial number through not incorporating Cessna Service Bulletin SB The approved Weight and Balance Manual: part number 75WB-00 (or later approved revision) is applicable to the Model 750 serial numbers and on and aircraft incorporating Cessna Service Bulletin SB The airplane must be loaded according to the appropriate FAA Approved Weight and Balance Manual. The list of equipment included in certificate empty weight must be provided for each airplane at the time of original certification: The certified empty weight and corresponding center of gravity location must include: Hydraulic fluid System A (Total) kg (35.56 lb) at cm ( in) System B (Total) 9.97 kg (21.97 lb) at cm ( in) Unusable Fuel-Wing kg (65.0 lb) at cm ( in) NOTE 1 Unusable Fuel-Center 6.80 kg (15.0 lb) at cm ( in) (cont.) Trapped Fuel kg (22.2 lb) at cm ( in)
8 CESSNA 10 October 2011 EA Sheet 8/9 Engine Unusable Oil 0.45 kg (1.0 lb) at cm ( in) Engine Usable Oil kg (45.8 lb) at cm ( in) (full) NOTE 2 NOTE 3 NOTE 4 Approved Brazilian Airplane Flight Manual 75BR-00 (or later revision) is applicable to the Model 750 serial number through not incorporating Cessna Service Bulletin SB The Brazilian Airplane Flight Manual, corresponds to the FAA approved Airplane Flight Manual: part number 75FMA-00 (or later approved revision) plus the supplement No. 20, is applicable to the Model 750 serial number and on and aircraft incorporating Cessna Service Bulletin The airplane must be operated according to the appropriate Approved Brazilian Airplane Flight Manual. Required Placards are translated to the Portuguese language and are listed in the Report H and were based in a CESSNA document and in the Chapter XI of the Airplane Maintenance Manual part number 75MM00 (or later approved revision). Approved Airworthiness Limitations for mandatory compliance retirement life or inspection are included in the Maintenance Manual (Instructions for Continued Airworthiness), part number 75MM00 (or later approved revision), Chapter 4, Airworthiness Limitations. The differences of the Brazilian airplanes in relation to the basic FAA type design are summarized below: 1 The Brazilian Airplane Flight Manual nr. 75BR-00 original dated 19 October 1998 and further revision is the AFM approved by ANAC. The Brazilian AFM nr. 75BR-00 includes the supplement 20 Airplanes Certified to Brazilian Configuration for the airplanes serial number through not incorporating Cessna Service Bulletin SB The Brazilian AFM for Model 750 serial number and on and aircraft incorporating Cessna Service Bulletin SB , are incorporated in the FAA approved Brazilian AFM part number 75BRA-00 (or later approved revision) except the supplement 20 Airplanes Certified to Brazilian Configuration. 2 Markings and placards approved are those listed in the paragraph 8 of the report nr. H Brazilian Requirements for the Acceptance of the Model 750 X. 3 ADF1 and respective indication are required to be fed the emergency bus bar according with Brazilian operating regulations RBHA/FAR (d). 4 For airplane with configuration of 10 or more passenger excluding seat pilots the following equipments are required to be installed: 4.1 Solid State Flight Data Recorder per RBHA/FAR Ground Proximity Warning System (GPWS) per RBHA/FAR Both equipments are provided per drawing nr Avionics, Brazil Certification Reference Kit. 5 In accordance with RBHA/FAR (c) a paint color limitation on upper surface of ailerons, spoilers, flaps and elevators with reflectance value of 26 or greater is requested through drawing nr Exterior Control Model 750 Brazilian ECR and through Maintenance Manual 750MM Chapter 4 Airworthiness Limitation. 6 An escape hatch handle was requested through RBHA/FAR (c) to be implemented per drawing nr Rev. N/C Escape Hatch Handle and Part List nr Rev. N/C Escape Hatch Handle. NOTE 5 All replacement seats (crew and passenger), although they may comply with TSO C127, must also be demonstrated to comply with requirements of RBHA/FAR , , and The foam cushion buildup of all seats (crew and passenger) may not be altered unless deviations in
9 CESSNA 10 October 2011 EA Sheet 9/9 the foam construction are demonstrated by tests to comply with the listed RBHA/FAR 25 paragraphs. The LH side facing seat lap belt shall have a buckle which opens from the left to right to prevent the buckle s own inertia from causing it to open. Any other configuration must be verified by dynamic requirements. NOTE 6 Two (2) Honeywell AZ-840 Micro Air Data Computers (MADC) are required equipment. Approved part numbers are listed in the following table: MADCPart Number Model 750-xxxx serial range Service Bulletin through 0041 N/A , -0002, through 0015 SB Rev 0, and on SB Rev 2 Aircraft with part number MADCs meet the initial airworthiness requirements for operation in Reduced Vertical Separation Minimum (RVSM) airspace. NOTE 7 Production Certificate No. 4 applies to Model 750 serial numbers , , , and on. NOTE 8 NOTE 9 Model 750 airplanes have been approved for high altitude operations (altitudes above feet), by Special Conditions. Any modifications to the pressure vessel must be approved in accordance with the requirements as show in the certification basis. This includes modifications, which could result in a pressure vessel opening, either through crack-growth or antenna loss, greater than 3.98 sq.in. The airplane is approved for Category II operations (flight-director autopilot-coupled only). This does not constitute operational approval. Minimum approved integrated computer (IC-800) software is Phase IV (P/N ). (General Manager, Aeronautical Product Certification)
Hawker Beechcraft Corporation on March 26, 2007
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A00010WI Revision 8 Hawker Beechcraft 390 March 26, 2007 TYPE CERTIFICATE DATA SHEET NO. A00010WI This data sheet, which is part of Type Certificate
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.073 for Beechcraft 390 (PREMIER I and IA) Type Certificate Holder: Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 USA For Models: Model 390 1
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION. TYPE CERTIFICATE DATA SHEET No. A50NM
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A50NM Dassault Aviation Falcon 2000 December 19, 1995 TYPE CERTIFICATE DATA SHEET No. A50NM This data sheet which is part of Type Certificate
More informationTYPE-CERTIFICATE DATA SHEET
TCDS No.: EASA.IM.A.207 Issue: 04 Date: 28 August 2018 TYPE-CERTIFICATE DATA SHEET No. EASA.IM.A.207 for CESSNA 500, 550, S550, 560, 560XL Type Certificate Holder: Textron Aviation Inc. One Cessna Boulevard
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A33EU
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A33EU Revision 2 DASSAULT-BREGUET Falcon 10 September 3, 1987 TYPE CERTIFICATE DATA SHEET NO. A33EU This data sheet which is a part of Type
More informationEuropean Aviation Safety Agency
TCDS No.: EASA.IM.A.212 Learjet M60 Page 1 of 15 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET No. EASA.IM.A.212 for LEARJET Model 60 Type Certificate Holder: Learjet Inc. One Learjet
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A18SW. San Antonio, Texas
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A18SW Revision 2 Fairchild Aircraft, Inc. SA227-CC SA227-DC (C-26B) November 14, 1996 TYPE CERTIFICATE DATA SHEET A18SW Type Certificate Holder:
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. T00009LA
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION T00009LA Revision 2 Marsh Aviation Company S-2F3AT November 18, 2002 TYPE CERTIFICATE DATA SHEET NO. T00009LA This data sheet, which is a part
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A49NM
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A49NM Jetcruzer 450 June 14, 1994 TYPE CERTIFICATE DATA SHEET NO. A49NM This data sheet which is a part of Type Certificate A49NM, prescribes
More informationFEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A8SW. San Antonio, Texas
FEDERAL AVIATION ADMINISTRATION A8SW Revision 21 Fairchild Aircraft SA226-TC SA227-AC (C-26A) SA227-PC SA227-BC (C-26A) February 6, 1997 TYPE CERTIFICATE DATA SHEET A8SW This data sheet, which is part
More informationCHAPTER 4 AIRWORTHINESS LIMITATIONS
Section Title CHAPTER 4 AIRWORTHINESS LIMITATIONS 4-10 Airworthiness Limitations..................................... 4.1 4-20 Additional Limitations....................................... 4.3 4-21 Parts
More informationEuropean Aviation Safety Agency
TCDS No.: TCDS IM.A.020 Learjet 45 Page 1 of 35 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET No. TCDS IM.A.020 for LEARJET MODEL 45 Type Certificate Holder: Learjet Inc. One Learjet
More informationREPUBLIC OF INDONESIA MINISTRY OF TRANSPORTATION DIRECTORATE GENERAL OF CIVIL AVIATION TYPE CERTIFICATE DATA SHEET NO. A094
REPUBLIC OF INDONESIA MINISTRY OF TRANSPORTATION DIRECTORATE GENERAL OF CIVIL AVIATION A094 Revision 0 Costruzioni Aeronautiche TECNAM S.r.L P2006T 7 June 2013 TYPE CERTIFICATE DATA SHEET NO. A094 This
More informationI - Model PZL SW-4 (Normal Category Rotorcraft), approved 26 August % Min. 100% 100% Gas Producer Speed (continuous)
TYPE CERTIFICATE DATA SHEET No. ER-2011T13 Type Certificate Holder: Wytwórnia Sprzętu Komunikacyjnego "PZL-Świdnik" S.A. Al. Lotników Polskich 1 21-045 Świdnik Poland ER-2011T13-00 Sheet 01 PZL-ŚWIDNIK
More informationEuropean Aviation Safety Agency
Page 1/8 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET Cirrus Design SF50 Type Certificate Holder: Cirrus Design Corporation 4515 Taylor Circle Duluth, Minnesota 55811 United States
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A16EA
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A16EA Revision 15 True Flight Holdings LLC AA-5, AA-5A, AA-5B AG-5B September 18, 2009 TYPE CERTIFICATE DATA SHEET NO. A16EA This data sheet,
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A11EA
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A11EA Revision 9 American General Aircraft Holding Co. AA-1 AA-1A AA-1B AA-1C June 7, 1995 TYPE CERTIFICATE DATA SHEET NO. A11EA This data sheet,
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13 1A13 Revision 27 Revo, Inc. COLONIAL C-1 COLONIAL C-2 LAKE LA-4 LAKE LA-4A LAKE LA-4P LAKE LA-4-200 LAKE
More informationPilatus Aircraft Ltd. P.O. Box 992 CH Stans SWITZERLAND
F -3 1 of 7 This Data Sheet which is a part of Type Certificate No. F -3 prescribes conditions and limitations under which the product, for which the Type Certification was issued, meets the airworthiness
More informationEuropean Aviation Safety Agency
TCDS No.:TCDSIM.A.020 Learjet 45 Page 1 of 24 Issue: 15 Date: 16 Sept. 2016 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET No. TCDS IM.A.020 for LEARJET MODEL 45 Type Certificate Holder:
More informationEuropean Aviation Safety Agency
TCDS IM.A.080 BD100-1A10 (Challenger 300) Page 1/11 Issue 3.0, 26 October 2010 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET IM.A.080 CHALLENGER 300 Manufacturer: BOMBARDIER INC. P.
More informationEuropean Aviation Safety Agency
Page 1 of 17 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.011 Extra Flugzeugproduktions- und Vertriebs GmbH Schwarze Heide 21 D-46569, Hünxe Germany For models: -500 Issue 24
More informationEuropean Aviation Safety Agency
TCDS IM.A.226 Cessna Aircraft Company Page 1 of 20 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Cessna Model 208 Type Certificate Holder: Cessna Aircraft Company P.O. Box 7704 Wichita,
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.512 for Bell 206/407 Series Type Certificate Holder Bell Helicopter Textron Canada Limited 12 800 rue de l Avenir Mirabel, Québec J7J 1R4, Canada For Models: 206A
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A13CE
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A13CE Revision 28 CESSNA 177 177A 177B November 16, 2010 TYPE CERTIFICATE DATA SHEET NO. A13CE WARNING: Use of alcohol-based fuels can cause
More informationTYPE-CERTIFICATE DATA SHEET
Issue: 03 Date: 25/07/2018 TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.636 for Model 3000 Type Certificate Holder Textron Aviation Defense LLC 9709 East Central 67206 Wichita, Kansas United States of America
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.503 for (King Air) Type Certificate Holder Textron Aviation Inc. Once Cessna BoulevardWichita, KS 67215 USA For models: C90A C90GT C90GTi TE.CERT.00048-001 European
More informationEuropean Aviation Safety Agency
TCDS EASA.A.109 ASI AVIATION Page 1 of 10 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.109 F 406 Type Certificate Holder : ASI AVIATION 14 allée René Fonck 51100 REIMS France
More informationEuropean Aviation Safety Agency
Page 1 of 10 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.IM.A.158 EMBRAER Type Certificate Holder: Embraer Embraer S.A. Av. Brig. Faria Lima. 2170 12227-901 São Jose dos Campos
More informationEuropean Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET EASA.A.155 FALCON 7X. DASSAULT AVIATION 9 Rond Point Marcel Dassault PARIS
TCDS A.155 Page 1/11 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET EASA.A.155 FALCON 7X DASSAULT AVIATION 9 Rond Point Marcel Dassault 75008 PARIS For models: FALCON 7X Issue 4.0: 20
More informationEuropean Aviation Safety Agency
Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET APM 20 and APM 30 series Type Certificate Holder: BP 1 Manufacturer: BP 1 For variants: APM 20 APM 30 Issue 3 : 23 December
More informationTYPE-CERTIFICATE DATA SHEET
SF340A, 340B TYPE-CERTIFICATE DATA SHEET No. EASA.A.068 for SF340A, 340B Type Certificate Holder: Saab AB 581 88 Linköping SWEDEN For Models: SF340A, 340B TE.CERT.00051-001 European Aviation Safety Agency,
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-804. Continental E165-2 (see Item 106 for optional engines)
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-804 Revision 14 LAND-AIR (TEMCO) (LUSCOMBE) 11A 11E April 6, 2005 AIRCRAFT SPECIFICATION NO. A-804 Type Certificate Holder Luscombe Aircraft
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A21CE
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A2CE A2CE Revision American Champion (Bellanca) (Champion) August 25, 997 This data sheet, which is part of
More informationEuropean Aviation Safety Agency
TCDS A.185 P2006T Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.185 P2006T Type Certificate Holder Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.003 for Type Certificate Holder Erickson Incorporated, DBA Erickson Air-Crane 3100 Willow Springs Road P.O. Box 3247 Central Point, Oregon, 97502-0010 U.S.A. For
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.520 for 505 Type Certificate Holder Bell Helicopter Textron Canada Ltd. 12 800, rue de l Avenir Mirabel, Québec J7J 1R4 Canada For Model: 505 TE.CERT.00049-001
More informationTYPE CERTIFICATE DATA SHEET 2A10
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 2A10 Revision 23 LAVIA S.A. PA-25 PA-25-235 PA-25-260 TYPE CERTIFICATE DATA SHEET 2A10 November 30, 2000 This data sheet which is a part of
More informationTYPE CERTIFICATE DATA SHEET 2A8
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET 2A8 2A8 Revision 20 LAVIA S.A. PA-25 PA-25-235 PA-25-260 November 30, 2000 This data sheet which is part of Type
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.A.607 for BS 115 Type Certificate Holder BLACKSHAPE S.P.A. Strada Statale 16 KM 841+900 70043 Monopoli (BA) ITALY For models: BS 115 TE.CERT.00048-001 European Aviation
More informationCHAPTER 3 LIFE-LIMITED COMPONENTS
CHAPTER 3 LIFE-LIMITED COMPONENTS Section Title 3.100 Life-Limited Components..................................... 3.1 3.110 Time-in-Service Records................................... 3.1 3.120 Fatigue
More informationTYPE-CERTIFICATE DATA SHEET
TCDS No.: EASA.A.069 SAAB 2000 TYPE-CERTIFICATE DATA SHEET No. EASA.A.069 for SAAB 2000 Type Certificate Holder: Saab AB 581 88 Linköping SWEDEN For Models: SAAB 2000 TE.CERT.00051-001 European Aviation
More informationEuropean Aviation Safety Agency
TCDS A.185 Tecnam P2006T Page 1 of 8 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET P2006T Type Certificate Holder: Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 5A5
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 5A5 Revision 30 Cessna (USAF 0-1A) 305A (USAF 0-1E) 305C (USAF 0-1G) 305D 305F April 4, 1994 AIRCRAFT SPECIFICATION NO. 5A5 Type Certificate
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A19SO
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A19SO Revison 14 Piper Aircraft, Inc PA-44-180 PA-44-180T TYPE CERTIFICATE DATA SHEET NO. A19SO October 28, 2014 This data sheet, which is part
More informationTYPE-CERTIFICATE DATA SHEET
TCDS No.:EASA.IM.A.013 Gulfstream 200 / Galaxy Issue: 03 Date: 03 July 2017 TYPE-CERTIFICATE DATA SHEET EASA.IM.A.013 for GULFSTREAM 200 / GALAXY Type Certificate Holder GULFSTREAM AEROSPACE LP (GALP P.O.
More informationEuropean Aviation Safety Agency
R-TCDS.A.014 Page 1/10 European Aviation Safety Agency EASA RESTRICTED TYPE-CERTIFICATE DATA SHEET EASA.A.014 AIRBUS A300-600ST Manufacturer: AIRBUS 1 Rond-point Maurice Bellonte 31707 BLAGNAC FRANCE For
More informationEuropean Aviation Safety Agency
TCDS EASA IM.A.157 Page 1/9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Embraer EMB-500 Manufacturer: Embraer Embraer SA Av. Brig. Faria Lima. 2170 12227-901 São Jose dos Campos SP
More informationCHAPTER 3 LIFE-LIMITED COMPONENTS
Section Title CHAPTER 3 LIFE-LIMITED COMPONENTS 3.000 Life-Limited Components...................................... 3.1 3.001 Introduction............................................. 3.1 3.002 Time-In-Service
More informationHamilton. Hamilton. Jet A/A1 (See Approved Flight Manual for additional fuels) Engine Limits: Gas Gen RPM % Ng (2006)
TCDS No A-14 Revision 16 Pacific Aerospace Ltd 750XL 14 June 2018 TYPE CERTIFICATE DATA SHEET No A-14 This data sheet which is part of Type Certificate No A-14 prescribes the conditions and limitations
More informationTYPE CERTIFICATE DATA SHEET 2A10
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 2A10 Revision 28 LAVIA ARGENTINA S.A. PA-25 PA-25-235 PA-25-260 TYPE CERTIFICATE DATA SHEET 2A10 July 2, 2013 This data sheet which is a part
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.120 for Type Certificate Holder Robinson Helicopter Company 2901 Airport Drive Torrance, CA 90505 U.S.A. For Models:, Alpha, Beta, Mariner TE.CERT.00049-001 European
More informationEuropean Aviation Safety Agency
TCDS EASA.IM.A.162 Page 1/9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Tupolev TU 204-120CE Manufacturer: Tupolev PSC 17, Tupolev Embankment 111250 Moscow Russia For model: TU 204-120CE
More informationEuropean Aviation Safety Agency
P2010 Page 1 of 10 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.576 P2010 Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli ITALIA Issue 01: 26 Sept 2014 Issue
More informationTYPE CERTIFICATE DATA SHEET NO. 2H2. Wilbarger County Airport Airport Drive Vernon, Texas 76384
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 2H2 Revision 23 BRANTLY (YHO 3BR) B-2 B-2A B-2B August 14, 2002 TYPE CERTIFICATE DATA SHEET NO. 2H2 This data sheet which is part of type certificate
More informationEuropean Aviation Safety Agency
TCDS IM.A.080 BD-100-1A10 Page 1/12 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET CHALLENGER 300 CHALLENGER 350 Manufacturer: BOMBARDIER INC. 800 Boul. René-Lévesque Ouest Montreal,
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.R.145 for Type Certificate Holder Hélicoptères Guimbal 1070, rue du Lieutenant Parayre Aérodrome d'aix-en-provence 13290 Les Milles France For Model: TE.CERT.00049-001
More informationEuropean Aviation Safety Agency
TCDS IM.A.211 Page 1/20 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA IM.A.211 MD-90-30, B717-200 McDonnell Douglas Corporation 3855 Lakewood Boulevard Long Beach, California 90846-0001
More informationEuropean Aviation Safety Agency
EASA.IM.A.191 Bombardier DHC-8 Page 1 of 34 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.IM.A.191 DHC-8 Type Certificate Holder: Bombardier Inc. 123 Garratt Boulevard Toronto,
More informationSection IV: Type Certificate Data Sheet and Specifications (TCDS)
Section IV: Type Certificate Data Sheet and Specifications (TCDS) TCDS Background Information A37C, Cessna 208 E4EA, Pratt & Whitney PT6A P9NE, Hartzell P60GL, McCauley E252, Continental C90 2A13, Piper
More informationAIR TRACTOR, INC. OLNEY, TEXAS
TABLE OF CONTENTS LOG OF REVISIONS... 2 DESCRIPTION... 4 SECTION 1 LIMITATIONS... 5 SECTION 2 NORMAL PROCEDURES... 8 SECTION 3 EMERGENCY PROCEDURES... 8 SECTION 4 MANUFACTURER'S SECTION - PERFORMANCE...
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION RESTRICTED AIRCRAFT SPECIFICATION NO. AR-7
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION RESTRICTED AIRCRAFT SPECIFICATION NO. AR-7 AR-7 Revision 10 PIPER PA-18A PA-18A "135" PA-18A "150" April 23, 1996 Type Certificate Holder The
More informationEuropean Aviation Safety Agency
TCDS No.: EASA.IM.A.526 EMB-550 Page 1 of 11 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET No. EASA.IM.A.526 for EMB-550 Type Certificate Holder: Embraer S.A. Av. Brigadeiro Faria Lima,2170.
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.121 for Type Certificate Holder Robinson Helicopter Company 2901 Airport Drive Torrance, CA 90505 U.S.A. For Models:, II TE.CERT.00049-001 European Aviation Safety
More informationEuropean Aviation Safety Agency
Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.583 Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli ITALIA Issue 01: 27 September 2013 TC issue Issue
More informationTYPE-CERTIFICATE DATA SHEET
TCDS IM.A.234 Piper PA-28 Page 1 of 15 TYPE-CERTIFICATE DATA SHEET No. EASA.IM.A.234 for Piper PA-28 Type Certificate Holder: Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida 32960 U.S.A. For
More informationFokker 50 - Limitations GENERAL LIMITATIONS MASS LIMITATIONS. Page 1. Minimum crew. Maximum number of passenger seats.
GENERAL LIMITATIONS Minimum crew Cockpit: Two pilots Maximum number of passenger seats Sixty-two (62) Maximum operating altitudes Maximum operating pressure altitude: Maximum take-off and landing pressure
More informationTCDS NUMBER E00078NE U.S. DEPARTMENT OF TRANSPORTATION REVISION: 3 DATE: April 12, 2011
TCDS NUMBER E00078NE U.S. DEPARTMENT OF TRANSPORTATION REVISION: 3 DATE: April 12, 2011 FEDERAL AVIATION ADMINISTRATION GENERAL ELECTRIC COMPANY MODELS: TYPE CERTIFICATE DATA SHEET E00078NE GEnx-1B54 GEnx-1B58
More informationCAP10. European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.370 CAP10. Type Certificate Holder CEAPR
Page 1 of 10 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.370 Type Certificate Holder 1 Route de Troyes 21121 DAROIS FRANCE For models: B Issue 07: 15 September 2016 EASA Form
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET NO. EASA.A.610 for Type Certificate Holder Game Composites Ltd. Ground Floor Flat 56 Queen s Gate, London, SW7 5JW, United Kingdom For models: TE.CERT.00048-001 European Aviation
More informationC.G. Range Fwd Limit 30.2 in AOD )All Aft Limit 33.8 in AOD Acrobatic )Weights 36.0 in AOD Normal ) Empty Weight C.G. Range
A-10 Revision 18 Pacific Aerospace Ltd CT/4 CT/4A CT/4B CT/4E 11 November 2015 TYPE CERTIFICATE DATA SHEET No A-10 This data sheet, which is part of Type Certificate No A-10, prescribes conditions and
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.113 for S-76 Series Type Certificate Holder Sikorsky Aircraft Corporation 6900 Main Street Stratford, Connecticut 06497-9129 U.S.A. For Models: S-76A S-76B S-76C
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A Piper Drive Vero Beach, Florida 32960
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1A6 Revision 33 PIPER PA-22 PA-22-108 PA-22-135 PA-22S-135 PA-22-150 PA-22S-150 PA-22-160 PA-22S-160 February 12, 1999 AIRCRAFT SPECIFICATION
More informationEuropean Aviation Safety Agency XA42
Page 1 of 13 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET A.507 XtremeAir GmbH Harzstrasse 2, Am Flughafen Cochstedt 39444 Hecklingen Germany For model: XA41 CONTENT Page 2 of 13 SECTION
More informationEuropean Aviation Safety Agency
TCDS A.412 Tecnam P92 Page 1 of 13 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.412 TECNAM P92 Type Certificate Holder: Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478
More informationEuropean Aviation Safety Agency
TCDS EASA.A.510 C.E.A.P.R. DR 200 Page 1 of 21 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.510 DR 200 series Type Certificate Holder: C.E.A.P.R. 1 route de Troyes 21121 DAROIS
More informationTYPE-CERTIFICATE DATA SHEET EASA.A.060. Ae 270
TCDS EASA.A.060 Ae 270 Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.060 Ae 270 Type Certificate Holder: AIRCRAFT INTEGRATED SOLUTIONS LTD International House 12 Constance
More informationTYPE-CERTIFICATE DATA SHEET
Page 1 of 9 TYPE-CERTIFICATE DATA SHEET EASA.A.583 Costruzioni Aeronautiche TECNAM S.r.l. Via Tasso, 478 80127 Napoli ITALIA EASA Form NR 90 CS-23 Issue 01 Page 2 of 9 CONTENT SECTION A: A.I. General A.II.
More informationEuropean Aviation Safety Agency
TCDS No.: IM.A.070 Gulfstream GII, GIII, GIV, GV Page 1 of 49 Issue 5.0 Date: 12 June 2013 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.IM.A.070 for GULFSTREAM GII, GIII, GIV &
More informationEuropean Aviation Safety Agency
TCDS EASA.A.191 Page 1/15 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Jetstream 3100 / 3200 Series Type Certificate Holder: BAE SYSTEMS (OPERATIONS) LTD Prestwick International Airport
More informationEuropean Aviation Safety Agency
Issue 16, 15 July, 2015 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET AB139 (from S/N 31001 up to S/N 31054) Name changed in AW139 (from S/N 31055 onwards) Type Certificate Holder: AGUSTAWESTLAND
More informationPage 1 of 7 01-Mar-2013 EASA.IM.A.341. Company. Be-103. Issue 2 EASA. Taganrog, BE-103. For models: general
Page 1 of 7 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.IM.A.341 BE-103 Type Certificate Holder: Berievv Aircraft Company 1,, Aviatorovv square Taganrog, 347923 RUSSIA For models:
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.103 for Model K-1200 Type Certificate Holder Kaman Aerospace Corporation P.O. Box 2, Old Windsor Road Bloomfield, Connecticut 06002 U.S.A. For Model: Model K-1200
More informationSECTION 2 LIMITATIONS
SECTION 2 TABLE OF CONTENTS PARAGRAPH PAGE 2.1 INTRODUCTION 2-1 2.2 KINDS OF OPERATIONS LIMITS 2-1 2.3 AIRSPEED 2-3 2.4 AIRSPEED INDICATOR MARKINGS 2-3 2.5 POWER PLANT 2-4 2.6 POWER PLANT INSTRUMENT MARKINGS
More informationTYPE-CERTIFICATE DATA SHEET
S205-S208 Page 1 TYPE-CERTIFICATE DATA SHEET No. EASA.A.587 S205 S208 Type Certificate Holder: LEONARDO S.p.A. Divisione Velivoli Piazza Monte Grappa, 4 00195 Rome Italy Airworthiness Category: Small Aeroplanes
More informationEASA TYPE-CERTIFICATE DATA SHEET EASA.A.113 IAR-46 / -46S
TCDS EASA.A.113 IAR-46/46S Page 1 of 8 EASA TYPE-CERTIFICATE DATA SHEET EASA.A.113 IAR-46 / -46S Type Certificate Holder: Aeroclubul Romaniei Bd.Lascar Catargiu, Nr.54, cod: 010673 Sector 1, Bucharest
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. IM.E.044 for AE 3007 Series Type Certificate Holder Rolls-Royce Corporation P.O. Box 420 Indianapolis, Indiana 46206-0420 United States of America For Models: AE 3007C AE
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.R.114 for Series Type Certificate Holder Leonardo S.p.A. Helicopters Piazza Monte Grappa, 4 00195 Roma Italy For Models: AB212 AB412, AB412 EP TE.CERT.00049-001 European
More informationEuropean Aviation Safety Agency
TCDS A.006 Tecnam P2002 Page 1 of 12 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET P2002 Manufacturer: Costruzioni Aeronautiche TECNAM S.r.l. Costruzioni Aeronautiche TECNAM S.r.l. Via
More informationTYPE CERTIFICATE DATA SHEET NO. A8SO
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A8SO Revision 21 (Pitts) S-1S S-1T S-2 S-2A S-2S S-2B S-2C February 15, 2005 TYPE CERTIFICATE DATA SHEET NO. A8SO This data sheet, which is
More informationEuropean Aviation Safety Agency: Ottoplatz 1, D Cologne, Germany - easa.europa.eu
EASA.A.539 Description: Language: TCDS: Product type: Manufacturer/TC Holder: A.539 Ruschmeyer R90 English EASA.A.539 Aircraft (CS-25, CS-22, CS-23, CS-VLA, CS-LSA) Bernd Hager/Anatoli Stobbe GbR European
More informationSECTION 2 LIMITATIONS
GENERAL This section includes operating limitations, instrument markings, and basic placards required for safe operation of the helicopter, its engine, and other standard systems. This helicopter is approved
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E4WE Revision 34 HONEYWELL (AlliedSignal, Garrett, AiResearch) TPE331-3 TPE331-8 TPE331-10N TPE331-11U TPE331-3U TPE331-8A TPE331-10P TPE331-11UA
More informationEuropean Aviation Safety Agency: Ottoplatz 1, D Cologne, Germany - easa.europa.eu
EASA.A.006 Description: Language: TCDS: Product type: Manufacturer/TC Holder: A.006 Tecnam P2002 English EASA.A.006 Aircraft (CS-25, CS-22, CS-23, CS-VLA, CS-LSA) TECNAM Costruzioni Aeronautiche European
More informationUNITED KINGDOM CIVIL AVIATION AUTHORITY
UNITED KINGDOM CIVIL AVIATION AUTHORITY BA 27 Issue 4 JETSTREAM 4100 TYPE CERTIFICATE DATA SHEET NO. BA27 This data sheet which is part of CAA Type Certificate No. BA27, prescribes conditions and limitations
More informationGACE Flying Club Aircraft Review Test 2018 N5312S & N5928E. Name: GACE #: Score: Checked by: CFI #:
GACE Flying Club Aircraft Review Test 2018 N5312S & N5928E Name: GACE #: Score: Checked by: CFI #: Date: (The majority of these questions are for N5312S. All N5928E questions will be marked 28E) 1. What
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A Himalaya Road Aurora, Colorado 80011
Type Certificate Holder: DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A-787 Univair Aircraft Corporation 2500 Himalaya Road Aurora, Colorado 80011 A-787
More informationCIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC
CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC 94-08 Revision 5 MORAVAN-AEROPLANES a.s. Z 143 L Z 143 LSi 15.07.2004 TYPE CERTIFICATE DATA SHEET No. 94-08 This data sheet which is a part of Type Certificate
More informationEuropean Aviation Safety Agency
EASA.IM.A.191 Bombardier DHC-8 Page 1 of 34 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.IM.A.191 DHC-8 Type Certificate Holder: Bombardier Inc. 123 Garratt Boulevard Toronto,
More informationDEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A-799. P.O. Box 7704 Wichita, Kansas 67277
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A-799 A-799 Revision 51 CESSNA 170 170A 170B July 15, 1998 Type Certificate Holder Cessna Aircraft Company P.O.
More information